The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Nov. 19, 2019

Filed:

Aug. 17, 2017
Applicant:

Bae Systems Information and Electronic Systems Integration Inc., Nashua, NH (US);

Inventors:

David J. Schorr, Austin, TX (US);

Jeremy B. Gibson, Bedford, NH (US);

James H. Steenson, New Boston, NH (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F41G 7/22 (2006.01); G05D 1/10 (2006.01); F41G 7/36 (2006.01); F42B 15/01 (2006.01); F42B 15/10 (2006.01); G06F 17/11 (2006.01);
U.S. Cl.
CPC ...
F41G 7/2213 (2013.01); F41G 7/36 (2013.01); F42B 15/01 (2013.01); F42B 15/10 (2013.01); G05D 1/108 (2013.01); G06F 17/11 (2013.01);
Abstract

A device, system, and method for shaping the trajectory of a projectile employing a Gravity bias, Gbias. The system includes a seeker, a guidance filter, a pitch rate filter, an actuator, pitch/yaw/roll coupled aerodynamics, and lateral rate sensors. It receives roll orientation input to a guidance and control autopilot; it applies Additional Gbias to that produced by the null rate command to the lateral control loops of the guidance and control autopilot device. The lateral rate command is equal to the desired Additional Gbias divided by an estimate of the projectile velocity. The Additional Gbias is translated to a rate command and incorporated into guidance loop commands to boost an Inherent Gbias to shape the trajectory of the projectile to the target.


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